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Connector adaptive plugging device

A self-adaptive, connector technology, applied in the direction of the launch device, can solve the problems of poor reliability, low operating efficiency, and high work intensity of assembly personnel, and achieve the effect of reducing work intensity, simple structure, and eliminating uncertain factors

Active Publication Date: 2016-12-14
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, because the assembly personnel need to manually realize the centering, insertion and installation and fixing of the plug on the four-bar linkage mechanism and the socket on the spring in the narrow installation space, there are low operating efficiency, poor reliability, and work intensity of the assembly personnel. many other issues

Method used

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Embodiment Construction

[0018] The following combination Figure 1 ~ Figure 2 , a preferred embodiment of the present invention is described in detail.

[0019] Such as figure 1 and figure 2 As shown, the connector adaptive mating device provided by the present invention realizes the automatic connection and separation between the missile 11 and the launch box 12, including: a four-bar linkage mechanism 3 fixedly arranged on the launch box 12 through the installation base 15 The linkage mechanism is connected between the four-bar linkage mechanism 3 and the missile 11; the plug 2 is fixedly arranged on the four-bar linkage mechanism 3; the socket 9 is fixedly arranged on the missile 11, and the The position of the socket 9 corresponds to the position of the plug 2; when the missile 11 is loaded or fired, the interlocking mechanism drives the plug 2 on the four-bar linkage mechanism 3 to self-fit or automatically separate from the socket 9 arranged on the missile 11 .

[0020] The linkage mechani...

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PUM

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Abstract

The invention relates to a connector adaptive plugging device to realize automatic connection and separation of a missile and a launcher container. The connector adaptive plugging device comprises a four-connecting rod mechanism fixedly disposed on the launcher container by means of a mounting base, an interlocking mechanism connected between the four-connecting rod mechanism and the missile, a plug fixedly disposed on the four-connecting rod mechanism, and a socket fixedly disposed on the missile and corresponding to the plug in position. During missile loading or launching, the plug on the four-connecting rod mechanism is driven by the interlocking mechanism to be adaptively plugged in or automatically separated from the socket disposed on the missile. The connector adaptive plugging device is capable of adaptively achieving plugging-in or separation of the missile and the launcher container under the circumstance that no any external force is used and the power is provided by the motion of the missile, and is simple in structure and high in reliability.

Description

technical field [0001] The invention relates to an insertion device, in particular to an adaptive insertion device for a missile connector. Background technique [0002] In the prior art, the detection and power supply of the missile in the launch box are all realized by falling off the plug and the socket. The socket is installed radially on the missile, and the plug is installed on the upper link of the four-bar linkage of the launch box. When the missile is launched, the connecting rods on both sides of the four-bar linkage mechanism are moved forward and downward by driving the guide pins on the plug, thereby realizing the separation of the plug and the socket. [0003] However, because the assembly personnel need to manually realize the centering, insertion and installation and fixing of the plug on the four-bar linkage mechanism and the socket on the spring in the narrow installation space, there are low operating efficiency, poor reliability, and work intensity of th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F7/00
CPCF41F7/00
Inventor 张保刚于喆胡洁李昱霖
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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